公开(公告)号：US20240124163A1

公开(公告)日：2024-04-18

申请号：US18084519

申请日：2022-12-19

Applicant: National Cheng Kung University

Inventor： Yueh-Heng Li ,  Yu-Ting Wu ,  Chao-Wei Huang ,  Wei-Cheng Lo ,  Hsun-Chen Hsieh ,  Ping-Han Huang ,  Yi-Long Huang ,  Sheng-Wen Liu ,  Wei-Cheng Lien

IPC: B64G1/40 ,  H02N11/00

CPC classification number: B64G1/409 ,  H02N11/006

Abstract: A magnetic multi-pole propulsion array system is applied to at least one external cathode and includes a plurality of magnetic multi-pole thrusters connected adjacent to each other. Each magnetic multi-pole thruster includes a propellant provider, a discharge chamber, an anode and a plurality of magnetic components. The propellant provider outputs propellant. The discharge chamber is connected with the propellant provider to accommodate the propellant. The anode is disposed inside the discharge chamber to generate an electric field. The plurality of magnetic components is respectively disposed on several sides of the discharge chamber. One of the several sides of the discharge chamber of the magnetic multi-pole thruster is applied for one side of a discharge chamber of another magnetic multi-pole thruster.

公开(公告)号：US20230202685A1

公开(公告)日：2023-06-29

申请号：US17822471

申请日：2022-08-26

Applicant: Alfred Dennis Belen, III

Inventor： Alfred Dennis Belen, III

IPC: B64G1/44 ,  B64G1/60 ,  B64G1/40

CPC classification number: B64G1/44 ,  B64G1/60 ,  B64G1/409

Abstract: A vehicle including a sealed container, a propulsion system with an intake and an exhaust affixed to an interior of the sealed container, an exhaust stream emitted from the exhaust, a thrust corridor within the sealed configured to channel the exhaust stream, and a return corridor configured to channel an intake stream into the intake of the propulsion system wherein the exhaust stream transforms into the intake stream after traveling a sufficient distance within the sealed container and the exhaust stream and intake stream generate a pressure differential within the sealed container wherein the pressure differential is sufficient to result in a movement of the vehicle relative to the vehicle's surroundings.

公开(公告)号：US20190210744A1

公开(公告)日：2019-07-11

申请号：US16332288

申请日：2016-12-06

Applicant: Mitsubishi Electric Corporation

Inventor： Shunichi KAWAMURA

IPC: B64G1/40 ,  B64G1/10 ,  B64G1/24 ,  B64G1/22

CPC classification number: B64G1/409 ,  B64G1/10 ,  B64G1/222 ,  B64G1/24 ,  B64G1/242

Abstract: An artificial satellite (100) includes two pointing mechanisms (110, 120). The pointing mechanisms respectively include main body side gimbals (111, 121), deployed booms (112, 122), thruster side gimbals (113, 114), and thruster groups (115, 125). The main body side gimbal connects the deployed boom to a satellite main body (130) and adjusts a direction of the deployed boom. The thruster side gimbal connects the thruster to the deployed boom and adjusts the direction of the thruster. Each gimbal is a two-axis gimbal.

公开(公告)号：US20180229864A1

公开(公告)日：2018-08-16

申请号：US15431823

申请日：2017-02-14

Applicant: Salvatore Cezar Pais

Inventor： Salvatore Cezar Pais

IPC: B64G1/40 ,  G01V7/04 ,  H05H3/04 ,  G01V7/00 ,  H01J61/16

CPC classification number: B64G1/409 ,  G01V7/005 ,  G01V7/04 ,  H01J61/16 ,  H05H1/2475 ,  H05H3/04

Abstract: A high frequency gravitational wave generator including a gas filled shell with an outer shell surface, microwave emitters, sound generators, and acoustic vibration resonant gas-filled cavities. The outer shell surface is electrically charged and vibrated by the microwave emitters to generate a first electromagnetic field. The acoustic vibration resonant gas-filled cavities each have a cavity surface that can be electrically charged and vibrated by acoustic energy from the sound generators such that a second electromagnetic field is generated. The two acoustic vibration resonant gas-filled cavities are able to counter spin relative to each other to provide stability, and propagating gravitational field fluctuations are generated when the second electromagnetic field propagates through the first electromagnetic field.

公开(公告)号：US20170313446A1

公开(公告)日：2017-11-02

申请号：US15141270

申请日：2016-04-28

Applicant: Salvatore Pais

Inventor： Salvatore Pais

IPC: B64G1/40

CPC classification number: B64G1/409

Abstract: A craft using an inertial mass reduction device comprises of an inner resonant cavity wall, an outer resonant cavity, and microwave emitters. The electrically charged outer resonant cavity wall and the electrically insulated inner resonant cavity wall form a resonant cavity. The microwave emitters create high frequency electromagnetic waves throughout the resonant cavity causing the resonant cavity to vibrate in an accelerated mode and create a local polarized vacuum outside the outer resonant cavity all.

公开(公告)号：US09712031B2

公开(公告)日：2017-07-18

申请号：US13944336

申请日：2013-07-17

Applicant: Harold Ellis Ensle

Inventor： Harold Ellis Ensle

IPC: H02K41/025 ,  F03H99/00 ,  H02J7/02 ,  B64G1/40

CPC classification number: H02K41/025 ,  B60L2200/26 ,  B64G1/409 ,  F03H99/00 ,  H02J7/025 ,  Y02T10/7005

Abstract: A system for propelling craft which is applicable in any environment. It employs an alternating magnetic field supplied by a coil. A parallel plate capacitor is situated so that the flux of the magnetic field flows between the plates of the capacitor. The capacitor is charged and discharged in synchronization with the alternating magnetic field. The changing magnetic field creates an electric field that applies a force to the charge in the plates which is then transferred to the body of the device. Any induced reactive electric force on the coil affects equally the protons and electrons in the wires of the coil creating the magnetic field, thus the force is non-reactive. At the same time, the changing electric field in the capacitor creates a magnetic field. The current in the coils and/or the surface current in the ferromagnetic material (if present) experiences a force from the magnetic field. The magnetic field created by these currents, however, has no free charge between the plates of the capacitor with which to react, thus this force is also non-reactive. The two forces are in opposite directions, but are not the same magnitude, thus the device is propelled in a single direction.

公开(公告)号：US20170149362A1

公开(公告)日：2017-05-25

申请号：US15422270

申请日：2017-02-01

Applicant: Richard Banduric

Inventor： Richard Banduric

IPC: H02N11/00 ,  H02K3/30 ,  H02K3/04 ,  H02K3/02

CPC classification number: H02N11/006 ,  B64G1/409 ,  H02K3/02 ,  H02K3/04 ,  H02K3/30 ,  H02N11/008

Abstract: In an example, a method includes interacting electric fields from charges in conductors in different inertial reference frames to effect motion. The example method implements the mathematical framework that divides electric fields from charges in different inertial reference frames into separate electric field equations in electrically isolated conductors. The example method may implement the interaction of these electric fields to produce a force on an assembly that can, by way of illustration, propel a spacecraft using electricity without other propellant(s).

公开(公告)号：US20170137153A1

公开(公告)日：2017-05-18

申请号：US15049022

申请日：2016-02-20

Applicant: J. A. Gonzalez Y Martin

Inventor： J. A. Gonzalez Y Martin

IPC: B64G1/40

CPC classification number: B64G1/409 ,  B64G1/407

Abstract: Use of laser light (3) for the propulsion of an object, wherein a laser source (2) shines at the object with laser light (3) or wherein the object is provided with a laser source (2) that emits laser light (3).

公开(公告)号：US20170067451A1

公开(公告)日：2017-03-09

申请号：US15121749

申请日：2015-02-24

Applicant: INNOVATIVE MOTION GMBH

Inventor： THOMAS LEBERER

IPC: F03G3/08 ,  B63B39/04 ,  B63G8/14 ,  B64G1/28

CPC classification number: F03G3/08 ,  B63B39/04 ,  B63G8/14 ,  B64G1/283 ,  B64G1/409 ,  F03G7/10 ,  Y10T74/18536

Abstract: The invention relates to a drive arrangement containing a rotational mass which is supported so as to be rotatable about a first axis, a bearing element supported so as to be rotatable about a second axis extending perpendicular to the first axis having a bearing for supporting the rotational mass, an oscillating body supported so as to be rotatable about a third axis perpendicular to the second axis having a bearing for supporting the bearing element, a drive provided on the oscillating body for generating a rotary movement of the bearing element about the second axis, a housing having a bearing for supporting the oscillating body, and a brake fixed to the housing for braking the rotary movement of the oscillating body in such a way that with each braking operation a driving force is transmitted to the housing.

Abstract translation: 本发明涉及一种驱动装置，其包括被支撑为可围绕第一轴线旋转的旋转质量块，支撑为能够围绕垂直于第一轴线延伸的第二轴线旋转的轴承元件，该轴承元件具有用于支撑转动的轴承 支撑成能够围绕垂直于第二轴线的第三轴线旋转的摆动体，该振动体具有用于支撑轴承元件的轴承，设置在振动体上用于产生轴承元件围绕第二轴线的旋转运动的驱动器， 具有用于支撑摆动体的轴承的壳体和固定到壳体的制动器，用于制动摆动体的旋转运动，使得在每个制动操作中将驱动力传递到壳体。

公开(公告)号：US20160368623A1

公开(公告)日：2016-12-22

申请号：US15251408

申请日：2016-08-30

Applicant: 8 Rivers Capital, LLC

Inventor： Miles R. Palmer

IPC: B64G1/00 ,  F41F1/00 ,  F41A1/04 ,  F42C11/00 ,  B64G1/40 ,  F02K9/95

CPC classification number: B64G1/409 ,  B64G1/002 ,  B64G1/402 ,  B64G1/406 ,  F02K9/95 ,  F41A1/04 ,  F41B6/00 ,  F41B6/006 ,  F41F1/00 ,  F41F3/04 ,  F41F3/0406 ,  F42B6/006 ,  F42B15/10 ,  F42B15/12 ,  F42C11/00 ,  F42C11/04

Abstract: The present disclosure relates to a launch system, a launch vehicle for use with the launch system, and methods of launching a payload utilizing the launch vehicle and/or the launch system. The disclosure can provide for delivery of the payload at a terrestrial location, an Earth orbital location, or an extraorbital location. The launch vehicle can comprise a payload, a propellant tank, an electrical heater wherein propellant, such as a light gas (e.g., hydrogen) is electrically heated to significantly high temperatures, an exhaust nozzle from which the heated propellant expands to provide an exhaust velocity of, for example, 7-16 km/sec, and sliding electrical contacts in electrical connection with the electrical heater. The launch vehicle can be utilized with the launch system, which can further comprise a launch tube formed of concentric electrically conductive tubes, as well as an electrical energy source, such as a battery bank and associated inductor.

Abstract translation: 本公开涉及一种发射系统，与发射系统一起使用的运载火箭，以及使用该运载火箭和/或发射系统发射有效载荷的方法。 本公开可以提供在地面位置，地球轨道位置或眶外位置处的有效载荷的传送。 运载火箭可以包括有效载荷，推进剂罐，电加热器，其中诸如轻质气体（例如氢气）的推进剂被电加热到显着高的温度，加热的推进剂从该喷嘴膨胀以提供排气速度 例如为7-16km / sec，以及与电加热器电连接的滑动电触头。 运载火箭可以与发射系统一起使用，其可以进一步包括由同心导电管形成的发射管，以及电能源，例如电池组和相关联的电感器。